View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65773U 26145.41620188 +.00000000 +00000-0 +49939-3 0 00006
2 65773 51.9035 46.3811 0000956 109.0380 251.0686 14.79923069 05
| Epoch (UTC): | 25 May 2026 09:59:19 |
| Eccentricity: | 0.0000956 |
| inclination: | 51.9035° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 46.3811° |
| argument of perigee: | 109.0380° |
| revolutions per day: | 14.79923069 |
| mean anomaly at epoch: | 251.0686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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